Caseless formed propellant powder charge

ABSTRACT

A caseless formed propellant powder charge including a shaped propellant powder charge having a central continuous recess or hole and a percussion-sensitive primer charge with an H-shaped cross section disposed in the recess. Preferably, the shaped propellant charge and the primer charge are fabricated from materials such as nitrocellulose, polyvinyl nitrate, nitroguanidine, penthrite, or mixtures thereof, and tetrazene or tetrazene tricinate, respectively. The compression and dimensioning of the various portions of the H-shaped primer charge may be modified to achieve the desired sensitivity.

United States Patent Gawlick et al.

CASELESS FORMED PROPELLANT POWDER CHARGE Inventors: Heinz Gawlick, Furth/Bay; Guenther Marondel, Erlangen, both of Germany Dynamit Nobel Aktiengesellschaft, Germany Filed: Feb. 26, 1974 Appl. No.: 445,896

Related U.S. Application Data Continuation of Ser. No. 163,173, July 16, 1971, abandoned.

Assignee:

Foreign Application Priority Data July 18, 1970 Germany 2035851 U.S. Cl. 102/100; 102/38; 102/45; lO2/DIG. 1

Int. Cl. F42B 1/00 Field of Search 102/100, 101, DIG. l, 38, 102/44, 45, 39, 99

References Cited UNITED STATES PATENTS l0/l907 Quinlan et a]. 102/38 Oct. 14, 1975 3,372,643 3/1968 Kvavle 102/99 3,580,180 5/1971 Gawlick... 3,645,207 2/1972 03111613 102/40 Primary ExaminerStephen C. Bentley Assistant Examiner-Harold Tudor Attorney, Agent, or FirmCraig & Antonelli 15 Claims, 3 Drawing Figures ",,l X l US. Patent Oct. 14, 1975 3,911,825

FIG. I l

INVENTORS HEINZ GAWLICK GUNTHER MARONDEL BY CrQAg ,QM6MQQQL 1r HLQl ATTORNEYS CASELESS FORMED PROPELLANT POWDER CHARGE This is a continuation of application Ser. No. 163,173, filed July 16, 1971, now abandoned.

This invention relates to a formed propellant powder charge including a shaped propellant powder charge of slow-burning or deflagrating explosive materials which do not tend toward detonation, such as nitrocellulose, polyvinyl nitrate, nitroguanidine, penthrite, etc. or mixtures thereof, particularly for commercial appliances, such as stud driving tools, impact tools, operating mechanisms, quick-action switches, or the like. The shaped propellant charge of the prior art is exemplified by applicants US. Pat. No. 3,580,180 issued May 25, 1971 in which the shaped propellant powder charge is provided with a preferably central continuous recess or hole in which a primer charge including impact ignitable powder, such as, for example, tetrazene or tetrazene tricinate is accommodated. These formed propellant powder charges constitute caseless propellant cartridges which burn without leaving any residue for commercial and industrial apparatus not employing a projectile for driving studs and the like. Such cartridges are ignited in substantially closed combustion chambers of the type disclosed in US. Pat. No. 3,283,657 to Kvavle, issued Nov. 8, 1966 in which the gases evolving from the deflagration of the cartridge are utilized to operate the device or tool.

The formed propellant powder charge can exhibit varying sizes and varying shapes, e.g., annular or polygonal, depending on the purpose for which it is employed. Advantageously, in the manufacture of the formed propellant powder charges, the central recesses of the shaped charges always exhibit the same diameter.

Varying the thickness, and thus the power, of the shaped propellant powder charges,'while keeping the outer diameter constant, correspondingly modifies the percussion sensitivity of the primer charge in the recess. An increase in thickness of the shaped propellant charge produces an increase in the thickness of the primer charge, whereby the sensitivity is reduced. Conversely, in case of a very thin shaped propellant powder charge, the amount of primer to be accommodated in the recess can be so small as to be insufficient for ignition.

It is an object of the present invention to overcome the abovedescribed disadvantages and to provide a possibility for varying the percussion sensitivity of the formed propellant powder charge. In accordance with the invention, this is accomplished in a shaped propellant powder charge having a central recess by forming the percussion-sensitive powder charge contained therein as a molded article, with an H-shaped cross section. Advantageously, the legs of the H-shaped profile are fashioned to correspond to the height of the shaped charge.

In accordance with another feature of the invention, the percussion or impact-sensitive primer charge is compressed more densely in the'zone of the central web than in the zone of the two legs of the I-I-shaped profile. In a molded article formed in this manner, the more strongly compressed central web serves solely for igniting the primer charge by percussion, whereas the less compressed legs serve for transmitting the ignition flame from the central web to the adjoining shaped propellantpowder charge. In addition to modifying the compression of the primer charge in the zone of the central web, the height of the central web can also be altered. By the varying the height of the central web, the desired or required sensitivity limit can be set for the primer charge of percussion-sensitive powder pressed in an I-I-profile.

In the manufacture of the formed propellant powder charge according to the present invention, the percussion-sensitive powder or primer charge is introduced into the central recess, core or opening of the shaped propellant powder charge in the moist or dry state. By inserting from both sides, respectively, a die having a smaller diameter than the recess, the primer charge in the central zone is compressed to form the central web. The superfluous primer charge is distributed toward the margin on all sides until it reaches the upper and/or lower edge of the shaped propellant powder charge. At this point, the primer charge is prevented from being pressed further outwardly beyond the edges of the shaped propellant charge by means of an appropriate tool. By conducting this pressing step, a profile of the compressed primer charge is obtained which has an H- shaped cross section and wherein the central web, in accordance with the controllable insertion paths of the dies, has a definite height and compression. The legs of the thus-formed profile are not as strongly compressed as the central web in this operation, so that the legs quickly transmit the ignition flame due to their greater porosity. In any event, the primer charge is still compressed to such an extent in the area of the legs that it is in sufficiently intimate contact with the inner side of the shaped propellant powder charge to insure a satisfactory friction seat in the recess of the shaped charge.

Various embodiments of the invention will be explained in greater detail below with reference to the attached drawings wherein:

FIG. 1 shows a cross section of a caseless formed propellant powder charge;

FIG. 2 is a top view of the formed propellant powder charge of FIG. 1; and

' FIG. 3 is a top view of a modified formed propellant powder charge.

Referring to the drawings, shaped propellant charge 1, which may be shaped by casting or compressed from porous powder, and preferably comprises single-base .or double-base nitrocellulose powders, is formed with continuous central recess 3 having diameter 6. The external shape of shaped propellant powder charge 1 can be varied in a multitude of ways, e.g., the annularcylindrical configuration of FIG. 2, the octagonal ring of FIG. 3, etc.

Primer charge 2 of a percussion-sensitive mixture, such as tetrazene and nitrocellulose, is accommodated in recess 3. The percussion-sensitive mixture is then compressed into a shaped article having I-l-shaped cross section profile with central web 2a and legs 2b. The ends of legs 2b are'flush, in each case, with the upper and lower edge, respectively, of shaped propellant powder charge 1. Height 4 and length or diameter 6 of central web 2a can be varied as desired. In other words, the sensitivity limit of the primer charge can be set with the aid of the height 4. By employing a primer charge of a commercially available primer composition made into a paste with nitrocellulose and having a compression of about 50 kp/cm to 500 kp/cm depending on the moisture of the composition, one obtains, for example, at a height of the web of 1.2 mm., a sensitivity limit of about 70 cm'kp and at a height of the web of 1.3 mm., a limit of about 80 cm'kp. A uniform quality of the H-shaped primer charge is insured, for instance, by the following manufacturing method. The pressing dies, not shown, have diameter 5 which is smaller than diameter 6 of the recess. Upon the introduction of the dies, only the powder between the dies is compressed toform central web 2a, and the superfluous powder escapes toward the sides up to the upper or lower edge of the shaped propellant powder charge. Central web 2a receives a specific compression and height which is reproducible as many times as desired by this process, whereas the excess amounts, which can also be distributed non-uniformly in quantity, are displaced into the lateral space of recess 3 forming legs 2b of the H- shaped profile. The height of central web 2a can be manufactured, for example, at a tolerance of 111.2 mm., and the sensitivity limit, fixed in a correspondingly accurate fashion.

In the preferred commercial field of application for the shaped propellant powder charge 1, a large range of variations exists for choice of diameter 6 of recess 3 and diameter 5 of central web 2a. A ratio of the two diameters with respect to each other in the range of from 2 1 to 2 1.8 has been found advantageous. Height 4 of the central web will preferably be about 0.25 mm. to 1.5mm. and, in this connection, will be independent of the height of shaped propellant powder charge 1. By the formation of primer charge 2 within recess 3, as provided by the present invention, it is thus possible to determine and vary the sensitivity limit by means of the configuration of central web 2a, at a constant diameter of recess 3, regardless of the height and outer diameter of shaped propellant powder charge 1. It is therefore possible to achieve a uniform quality of formed propellant powder charges with primer charge, as well as the adaptation thereof to varying ignition or priming conditions.

Although only two embodiments have been specifically described and shown in the attached drawings, as is readily apparent to one skilledin the art, further embodiments, variations and changes may be made within the scope of the invention.

We claim:

1. A caseless propellant charge for commercial apparatus not employing a projectile for driving studs and the like comprising a shaped propellant powder charge defining a hole of a given width extending therethrough, and a percussion-sensitive primer ignitor charge of substantially the same width as 'said defined hole and secured therein, said percussion-sensitive primer ignitor charge having an H-shaped cross section taken parallel to the axis of said hole with two substantially parallel legs extending in the axial direction of said hole and a transversely extending web interconnecting said two legs at points intermediate the end of said legs.

2. The propellant charge of claim 1 wherein said shaped propellant powder charge includes a compound selected from the group consisting essentially of nitrocellulose, polyvinyl nitrate, nitroguanidine, penthrite and mixtures thereof.

3. The propellant charge of claim 1 wherein said percussion-sensitive primer charge includes a compound selected from the group consisting essentially of tetrazene and tetrazene tricinate.

4. The propellant charge of claim 1 wherein the length of the two legs of said H-shaped cross section of said percussion-sensitive primer charge are equal to the length of said hole.

5. The propellant charge of claim 1 wherein said percussion-sensitive primer charge is a compressed mixture.

6. The propellant charge of claim 5 wherein the central web portion of said l-l-shaped cross section is of greater compression density than are the two legs thereof.

7. The propellant charge of claim 1 wherein said shaped propellant powder charge is annularly-shaped and said percussion-sensitive primer charge circumferentially contacts the interior of said shaped propellant powder charge.

8. The propellant charge of claim 7 wherein the ratio between the diameters of said hole and the central web of said H-shaped cross section is in the range of from about 2: 1 to about 2: 1.8.

9. The propellant charge of claim 8 wherein the thickness of said central web is from about 0.25 mm.

to about 1.5 mm.

10. The propellant charge of claim 1, wherein said web is provided with a greater percussion-sensitivity than said legs of said H-shaped cross section, thereby determining the percussion-sensitivity of said primer ignitor charge.

11. The propellant charge of claim 10, wherein said percussion-sensitive primer-ignitor charge is formed of a percussion-sensitive compressed mixture, and wherein at least one of the density and the thickness of said compressed mixture at said web determines the percussion-sensitivity thereof, at least one of the density and thickness of said web being variable.

12. The propellant charge of claim 1, wherein said legs contact said shaped propellant charge, and wherein said web serves for igniting said primer ignitor charge by percussion and said legs serve for transmitting the igniting flame to the adjoining shaped propellant powder charge.

13. The propellant charge of claim 1, wherein the ends of said legs at said percussion-sensitive primerignitor charge lie in the same plane as the ends of the shaped propellant powder charge having the hole therethrough.

14. The propellant charge of claim 1, wherein the propellant charge is arranged for accommodation in a substantially closed combustion chamber whereupon ignition of the propellant charge, the gases generated upon deflagration of the charge are utilized to operate an explosive actuated device.

15. The propellant charge of claim 1, wherein the primer-ignitor charge has a percussion-sensitivity of about -80 cm-kp at the web thereof and the remaining portions of the propellant charge have a higher percussion-sensitivity. 

1. A caseless propellant charge for commercial apparatus not employing a projectile for driving studs and the like comprising a shaped propellant powder charge defining a hole of a given width extending therethrough, and a percussion-sensitive primer ignitor charge of substantially the same width as said defined hole and secured therein, said percussion-sensitive primer ignitor charge having an H-shaped cross section taken parallel to the axis of said hole with two substantially parallel legs extending in the axial direction of said hole and a transversely extending web interconnecting said two legs at points intermediate the end of said legs.
 2. The propellant charge of claim 1 wherein said shaped propellant powder charge includes a compound selected from the group consisting essentially of nitrocellulose, polyvinyl nitrate, nitroguanidine, penthrite and mixtures thereof.
 3. The propellant charge of claim 1 wherein said percussion-sensitive primer charge includes a compound selected from the group consisting essentially of tetrazene and tetrazene tricinate.
 4. The propellant charge of claim 1 wherein the length of the two legs of said H-shaped cross section of said percussion-sensitive primer charge are equal to the length of said hole.
 5. The propellant charge of claim 1 wherein said percussion-sensitive primer charge is a compressed mixture.
 6. The propellant charge of claim 5 wherein the central web portion of said H-shaped cross section is of greater compression densitY than are the two legs thereof.
 7. The propellant charge of claim 1 wherein said shaped propellant powder charge is annularly-shaped and said percussion-sensitive primer charge circumferentially contacts the interior of said shaped propellant powder charge.
 8. The propellant charge of claim 7 wherein the ratio between the diameters of said hole and the central web of said H-shaped cross section is in the range of from about 2 : 1 to about 2 : 1.8.
 9. The propellant charge of claim 8 wherein the thickness of said central web is from about 0.25 mm. to about 1.5 mm.
 10. The propellant charge of claim 1, wherein said web is provided with a greater percussion-sensitivity than said legs of said H-shaped cross section, thereby determining the percussion-sensitivity of said primer ignitor charge.
 11. The propellant charge of claim 10, wherein said percussion-sensitive primer-ignitor charge is formed of a percussion-sensitive compressed mixture, and wherein at least one of the density and the thickness of said compressed mixture at said web determines the percussion-sensitivity thereof, at least one of the density and thickness of said web being variable.
 12. The propellant charge of claim 1, wherein said legs contact said shaped propellant charge, and wherein said web serves for igniting said primer ignitor charge by percussion and said legs serve for transmitting the igniting flame to the adjoining shaped propellant powder charge.
 13. The propellant charge of claim 1, wherein the ends of said legs at said percussion-sensitive primer-ignitor charge lie in the same plane as the ends of the shaped propellant powder charge having the hole therethrough.
 14. The propellant charge of claim 1, wherein the propellant charge is arranged for accommodation in a substantially closed combustion chamber whereupon ignition of the propellant charge, the gases generated upon deflagration of the charge are utilized to operate an explosive actuated device.
 15. The propellant charge of claim 1, wherein the primer-ignitor charge has a percussion-sensitivity of about 70-80 cm.kp at the web thereof and the remaining portions of the propellant charge have a higher percussion-sensitivity. 